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Fretting fatigue in overhead conductors: Rig design and failure analysis of a Grosbeak aluminium cable steel reinforced conductor

机译:架空导体的微动疲劳:Grosbeak铝电缆钢增强导体的钻机设计和失效分析

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The performance optimisation of overhead conductors depends on the systematic investigation of the fretting fatigue mechanisms in the conductor/clamping system. As a consequence, a fretting fatigue rig was designed and a limited range of fatigue tests was carried out at the middle high cycle fatigue regime in order to access an exploratory S-N curve for a Grosbeak conductor, which was mounted on a mono-articulated aluminium clamping system. Subsequent to these preliminary fatigue tests, the components of the conductor/clamping system, such as ACSR conductor, upper and lower clamps, bolt and nuts, were subjected to a failure analysis procedure in order to investigate the metallurgical free variables interfering on the fatigue test results, aiming at the optimisation of the testing reproducibility. The results indicated that the rupture of the planar fracture surfaces observed in the external Al strands of the conductor tested under lower bending amplitude (0.9 mm) occurred by fatigue cracking (1 mm deep), followed by shear overload. The V-type fracture surfaces observed in some Al strands of the conductor tested under higher bending amplitude (1.3 mm) were also produced by fatigue cracking (approximately 400 mu m deep), followed by shear overload. Shear overload fracture (45 deg fracture surface) was also observed on the remaining Al wires of the conductor tested under higher bending amplitude (1.3 mm). Additionally, the upper and lower AJ-cast clamps presented microstructure-sensitive cracking, which was folowed by particle detachment and formation of abrasive debris on the clamp/conductor tribo-interface, promoting even further the fretting mechanism. The detrimental formation of abrasive debris might be inhibited by the selection of a more suitable class of as-cast Al alloy for the production of clamps. Finally, the boltut system showed intense degradation of the carbon steel nut (fabricated in ferritic-pearlitic carbon steel, featuring machined threads with 190 HV), with intense plastic deformation and loss of material. Proper selection of both the bolt and nut materials and the finishing processing might prevent the loss in the clamping pressure during the fretting testing. It is important to control the specification of these components (clamps, bolt and nuts) prior to the start of large scale fretting fatigue testing of the overhead conductors in order to increase the reproducibility of this assessment.
机译:架空导体的性能优化取决于对导体/夹紧系统中的微动疲劳机理的系统研究。因此,设计了微动疲劳试验台,并在中高周疲劳状态下进行了有限范围的疲劳测试,以获取安装在单铰链式铝制夹具上的Grossbeak导体的探索性SN曲线。系统。在这些初步疲劳测试之后,对导体/夹紧系统的组件(如ACSR导体,上下夹具,螺栓和螺母)进行了故障分析程序,以研究会干扰疲劳测试的冶金自由变量结果,旨在优化测试的可重复性。结果表明,在较低弯曲幅度(0.9毫米)下测试的导体的外部铝绞线中观察到的平面断裂表面的断裂是由疲劳裂纹(1毫米深)引起的,然后是剪切过载。在较高弯曲幅度(1.3毫米)下测试的导体的某些铝绞线中观察到的V型断裂表面也是由疲劳裂纹(约400微米深)产生的,随后是剪切过载。在较高弯曲幅度(1.3毫米)下测试的导体的其余铝线上也观察到了剪切过载断裂(45度断裂面)。此外,上部和下部的AJ浇铸夹具呈现出对微观结构敏感的开裂,这是由于在夹具/导体的摩擦界面上出现了颗粒分离和磨料碎片的形成,进一步促进了微动机理。磨料碎片的有害形成可以通过选择一种更合适的用于铸造夹具的铸态铝合金来抑制。最后,螺栓/螺母系统显示出碳素钢螺母(用铁素体-珠光体碳素钢制成,具有加工190 HV的机加工螺纹)的强烈降解,并产生强烈的塑性变形和材料损失。正确选择螺栓和螺母的材料以及进行精加工可能会防止在微动试验期间夹紧压力的损失。在开始对架空导体进行大规模微动疲劳测试之前,控制这些组件(夹具,螺栓和螺母)的规格很重要,这样才能提高评估的可重复性。

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